Grant: Alliance Grants
University of Victoria
$270,000.00
PredictiOn, Assessment and ExpeRimental Validation of AeroservoelastiC Tools and Processes in Design of Novel and Flexible AIRcraft Configurations [ORCA-AIR]
EF 2023-24
Résumé
There are conflicting challenges in aeronautics. On one side, air traffic is growing, with the need to increase capacity and reduce travel time while maintaining or improving safety, and concurrently reduce emissions to mitigate climate change. It is evident that evolutionary solutions will not suffice to meet the challenging targets in terms of environmental impact reduction, while ensuring competitiveness of the Canadian aviation and associated supply chain industries. In the search for revolutionary solutions, ORCA-AIR proposes to leverage the knowledge, expertise and experimental facilities in 'design, build, test and fly' to buttress the development of green aviation with the development of an aerodynamically efficient blended-wing-body aircraft configuration.ORCA-AIR is proposing to study the blended-wing-body aircraft configuration that will impact on two significant levers for reduction of fuel burn needed for future clean aviation: improved aerodynamics and weight reduction. The lightweight blended-wing-body configuration has been shown to reduce drag and improve lift thus contributing to emissions reduction. More specifically, the goal is to characterize the aeroservoelastic behaviour of a BWB with flexible wings to achieve key performance, stability and control requirements, while improving energetic efficiency.
Programme
Alliance Grants
Bénéficiaire
Emplacement
British Columbia, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
578448-2022
Name nom
Suleman, Afzal A
Department département
Mechanical Engineering
Organization id
7
Institution établissement
University of Victoria
Province en
British Columbia
Province fr
Colombie-Britannique
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2023
Competition year année de concours
2022
Award amount
270000
Program id
ALLRP
Program name en
Alliance Grants
Program name fr
Subventions Alliance
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2108
Research subject group en
Mechanical engineering
Research subject group fr
Aerospace, aeronautical and automotive engineering
Research subject en
Génie mécanique
Research subject fr
Génie aérospatial, aéronautique et automobile
Application title
PredictiOn, Assessment and ExpeRimental Validation of AeroservoelastiC Tools and Processes in Design of Novel and Flexible AIRcraft Configurations [ORCA-AIR]
Keyword
Aeroservoelasticity; Aircraft Design; Flight Control Systems; Flight Testing; Novel Aircraft Configurations
Application summary
There are conflicting challenges in aeronautics. On one side, air traffic is growing, with the need to increase capacity and reduce travel time while maintaining or improving safety, and concurrently reduce emissions to mitigate climate change. It is evident that evolutionary solutions will not suffice to meet the challenging targets in terms of environmental impact reduction, while ensuring competitiveness of the Canadian aviation and associated supply chain industries. In the search for revolutionary solutions, ORCA-AIR proposes to leverage the knowledge, expertise and experimental facilities in 'design, build, test and fly' to buttress the development of green aviation with the development of an aerodynamically efficient blended-wing-body aircraft configuration.ORCA-AIR is proposing to study the blended-wing-body aircraft configuration that will impact on two significant levers for reduction of fuel burn needed for future clean aviation: improved aerodynamics and weight reduction. The lightweight blended-wing-body configuration has been shown to reduce drag and improve lift thus contributing to emissions reduction. More specifically, the goal is to characterize the aeroservoelastic behaviour of a BWB with flexible wings to achieve key performance, stability and control requirements, while improving energetic efficiency.